connor/thesis
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

Maybe nearing the final commit

Browse Source
This commit is contained in:
Connor
2022-04-18 10:59:25 -06:00
parent 0fb875c777
commit 5b6656a9a6
3598 changed files with 79349 additions and 572 deletions
Download Patch File Download Diff File Expand all files Collapse all files

22
archive/ES_0.5624989423538167 Normal file
View File

@@ -0,0 +1,22 @@
archive/ES_0.5624989423538167---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-04-30T21:12:32.324
Launch V∞: [6.513114762320057, -7.463953934913978, 0.1859439381831087] km/s
Phase 1:
Planet: Saturn
V∞_in: [-4.316204368127439e-6, 4.1735553538676255e-6, 4.844313279529403e-6] km/s
V∞_out: [6.43257282693189e-6, 4.256614393877074e-6, 1.5086104159405055e-7] km/s
time of flight: 1.8353695539817083e8 seconds
arrival date: 2029-02-22T03:41:47.324
thrust profile: [0.21317491471510075 -0.06229395613773833 -0.07940076174166129; 0.021291590834692595 0.004490438208634555 -0.025108403921017895; 0.06788369572747571 0.030191089739782455 -0.1276974257438681; 0.05601098014271953 0.033482657689394894 -0.146453644931716; 0.047309378460901864 0.0338630308302544 -0.15731089089216455; 0.037390980042361154 0.030372343987206007 -0.15072536637745163; 0.01540558281930896 0.013693073048598275 -0.07431284895797785; 0.008682421137620203 0.008228903260804875 -0.04812275982346394; 0.004568843898098114 0.00456618001922739 -0.028738532475996784; 0.007338506692526304 0.007793613390244167 -0.04932287207318788; 0.002022230952246362 0.0021816571610006174 -0.013845957991670236; 0.00020696707412351653 1.979823262693377e-5 -0.0016328705339009259; 0.0012514057141636557 -0.00014126208962748297 -0.0028725515708376854; 0.0002563547853994605 6.153281503670625e-5 -0.0011532669118436522; -0.00090198382072105 0.0023459618187470473 -0.0011877352270692127; 5.0448616446754566e-5 -0.00011701969707143844 -0.001886971819526469; 0.00013869821520981257 -0.0010620438849940953 -0.0006948379717578684; -0.0009297167730377544 -0.0016126871557369847 -0.0006580701035986466; 0.0007445880288685402 0.0004467911073203005 -0.004544137968190991; -0.0006641235483207195 -0.000810086354436365 0.0013223781671552995] %
Mass Used: 83.6146562588574 kg
Launch C3: 98.16584739781635 km²/s²
||V∞_in||: 7.714632563477306e-6 km/s